BRPI0817758A2 - Airframe fuselage structure for composite material aircraft fuselage, and, aircraft - Google Patents

Airframe fuselage structure for composite material aircraft fuselage, and, aircraft

Info

Publication number
BRPI0817758A2
BRPI0817758A2 BRPI0817758A BRPI0817758A2 BR PI0817758 A2 BRPI0817758 A2 BR PI0817758A2 BR PI0817758 A BRPI0817758 A BR PI0817758A BR PI0817758 A2 BRPI0817758 A2 BR PI0817758A2
Authority
BR
Brazil
Prior art keywords
aircraft
fuselage
composite material
fuselage structure
airframe
Prior art date
Application number
Other languages
Portuguese (pt)
Inventor
Guillaume Gallant
Laurent Giuseppin
Damien Aguera
Original Assignee
Airbus Operations Sas
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI0817758A2 publication Critical patent/BRPI0817758A2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

A fuselage structure for an aircraft fuselage in composite material and an aircraft including such a fuselage structure. The fuselage structure provides savings in mass while allowing grounding of electric systems, and with which substantial mechanical stiffness characteristics may be guaranteed. In the fuselage structure attachment modules provide an assembling function as well as an electric function.
BRPI0817758 2007-10-08 2008-09-29 Airframe fuselage structure for composite material aircraft fuselage, and, aircraft BRPI0817758A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0758132A FR2921898B1 (en) 2007-10-08 2007-10-08 FUSELAGE STRUCTURE FOR AIRCRAFT FUSELAGE IN COMPOSITE MATERIAL AND AIRCRAFT EQUIPPED WITH SUCH A FUSELAGE STRUCTURE
PCT/EP2008/063018 WO2009047158A1 (en) 2007-10-08 2008-09-29 Fuselage structure for aircraft fuselage made of composite material and aircraft equipped with such fuselage structure

Publications (1)

Publication Number Publication Date
BRPI0817758A2 true BRPI0817758A2 (en) 2015-03-24

Family

ID=39473966

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0817758 BRPI0817758A2 (en) 2007-10-08 2008-09-29 Airframe fuselage structure for composite material aircraft fuselage, and, aircraft

Country Status (10)

Country Link
US (1) US8550399B2 (en)
EP (1) EP2197739B1 (en)
JP (1) JP5462174B2 (en)
CN (1) CN101821161B (en)
AT (1) ATE510766T1 (en)
BR (1) BRPI0817758A2 (en)
CA (1) CA2701690A1 (en)
FR (1) FR2921898B1 (en)
RU (1) RU2473452C2 (en)
WO (1) WO2009047158A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2952905B1 (en) * 2009-11-20 2012-06-01 Airbus Operations Sas DEVICE FOR ATTACHING STIFFENING MEANS TO A FRAME ELEMENT, AND STRUCTURE COMPRISING SUCH AN ATTACHING DEVICE
JP5808111B2 (en) 2011-02-04 2015-11-10 三菱重工業株式会社 Composite structure for aircraft, aircraft main wing and aircraft fuselage provided with the same
FR2984845B1 (en) * 2011-12-21 2014-07-11 Airbus Operations Sas ANTI-SPEED AIRCRAFT FUSELAGE STRUCTURE ELEMENT
RU2595354C1 (en) * 2015-05-21 2016-08-27 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Hypersonic aircraft body and method of making same
CN107434031A (en) 2016-05-25 2017-12-05 空中客车简化股份公司 The structure member of aircraft wing body and the aircraft including the structure member
RU2694638C2 (en) * 2017-11-09 2019-07-16 Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" Fuselage caisson
RU202616U1 (en) * 2020-11-02 2021-03-01 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" Aircraft fuselage from truss filler

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2489779A1 (en) * 1980-09-09 1982-03-12 Aerospatiale FUSELAGE STRUCTURE FOR AN AIRCRAFT RESISTANT TO THE LONGITUDINAL BREAKAGE OF THE EXTERIOR COATING
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
FR2693976B1 (en) * 1992-07-22 1994-09-30 Eurocopter France Fuselage structure for helicopter.
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
JP4318381B2 (en) * 2000-04-27 2009-08-19 本田技研工業株式会社 Manufacturing method of fuselage structure made of fiber reinforced composite material, and fuselage structure manufactured thereby
EP1336469A1 (en) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
DE102004001049B4 (en) * 2004-01-05 2009-12-10 Airbus Deutschland Gmbh Isolierpaket arrangement for the inner insulation of an aircraft fuselage
DE102004001078B8 (en) * 2004-01-05 2013-06-13 Airbus Operations Gmbh fuselage
RU2270135C2 (en) * 2004-03-04 2006-02-20 Карклин Андрей Михайлович Flying vehicle fuselage
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
FR2894869B1 (en) 2005-12-20 2009-10-09 Airbus France Sas METHOD FOR MANUFACTURING AIRCRAFT FUSELAGE OF COMPOSITE MATERIAL
US7277266B1 (en) * 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure

Also Published As

Publication number Publication date
JP5462174B2 (en) 2014-04-02
FR2921898B1 (en) 2009-12-11
RU2010117200A (en) 2011-11-20
US8550399B2 (en) 2013-10-08
FR2921898A1 (en) 2009-04-10
CN101821161A (en) 2010-09-01
CA2701690A1 (en) 2009-04-16
CN101821161B (en) 2013-02-13
JP2010540348A (en) 2010-12-24
EP2197739B1 (en) 2011-05-25
EP2197739A1 (en) 2010-06-23
US20100264273A1 (en) 2010-10-21
WO2009047158A1 (en) 2009-04-16
ATE510766T1 (en) 2011-06-15
RU2473452C2 (en) 2013-01-27

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.